Mechanical Engineering Questions And Answers :: Compressors: part5



Mechanical Engineering : Compressors QUESTIONS AND ANSWERS :: part5 : 6 to 10

Following Mechanical Engineering Multiple choice objective type questions and answers will help you in BSNL JTO, GATE 2024 and IES 2024 examinations :

6.Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

higher
lower
equal
can't be compared
unpredictable.

7.A gas turbine used in air craft should have

high h.p. and low weight
low weight and small frontal area
small frontal area and high h.p.
high speed and high h.p.
all of the above.

8.The maximum combustion pressure in gas turbine as compared to I.C. engine is

more
less
same
depends on other factors
unpredictable.

9.For an irreversible gas turbine cycle, the efficiency and work ratio both depend on

pressure ratio alone
maximum cycle temperature alone
minimum cycle temperature alone
both pressure ratio and maximum cycle temperature
none of the above.

10.The ideal efficiency of simple gas turbine cycle depends on

pressure ratio
maximum cycle temperature
minimum cycle temperature
all of the above
none of the above.

More Compressors QUESTIONS AND ANSWERS available in next pages

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